[fltsim.0]
title=Dewoitine_D338
sim=Dewoitine_D338
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=Dewoitine
ui_type=D-338
ui_variation=Air France
description="Dewoitine D338, French liner, 1938"
[General]
atc_type=Trimotor
atc_model=
editable=0
performance="Dewoitine D-338\nFrench Liner\n12 to 22 seats\nLength: 72,6 ft (22.13 m)\nSpan: 96,39 ft (29.38 m)\nEmpty weight: 7,905 kg\nTotal weight : 11,150 kg\nMax speed: 310 km/h\nCruise speed : 260 km/h\nCeiling : 4900 m\nRange : 2060 km\nEngines : 3 x 650 hp Hispano-Suiza 9V-17\n1st flight : August 9th, 1935\nModel by Patrice Grange, February 2008"
[CameraDefinition.0]
Title=Train d'atterrissage
Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description=Vue du train d'atterrissage sous l'aile gauche
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.52
ShowWeather=Yes
InitialXyz=-2.2, -1.2, -7
InitialPbh=0, 0, 13
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title=Empennage
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Vue de l'arrière de l'avion
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.75
ShowWeather=Yes
InitialXyz=0, 2, -25.0
InitialPbh=5, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.2]
Title=Aile droite
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Vue de droite
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=17, 1.6, -3.0
InitialPbh=6, 0, 280
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[weight_and_balance]
max_gross_weight = 19470
empty_weight = 11770
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 14885.4
empty_weight_roll_MOI = 13264.7
empty_weight_yaw_MOI = 28402.6
empty_weight_coupled_MOI = 0
max_number_of_stations = 8
station_load.0 = "170.0, 4.9, -1.5, 1.0, Pilot"
station_load.1 = "170.0, 4.9, 1.5, 1.0, Co-Pilot"
station_load.2 = "0.0, -2.0, -1.5, 0.0, Passenger 3"
station_load.3 = "170.0, -2.0, 1.5, 0.0, Passenger 4"
station_load.4 = "0.0, -6.8, -1.5, 0.0, Passenger 7"
station_load.5 = "0.0, -6.8, 1.5, 0.0, Passenger 8"
station_load.6 = "0.0, -7.9, -1.5, 0.0, Passenger 9"
station_load.7 = "250.0, -10.2, 0.0, 0.0, Baggage"
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//1 Longitudinal - minus rear (feet)
//2 Lateral - minus left (feet)
//3 elevation - minus lower (feet)
light.0 = 3, 5.92, -49.68, 2.53, fx_navred ,
light.1 = 3, 5.92, 49.68, 2.53, fx_navgre ,
light.2 = 4, 18.33, 0.00, 2.25, fx_vclight ,
light.3 = 4, 5.00, 0.00, 1.40, fx_vclight ,
light.4 = 4, -7.00, 0.00, 1.40, fx_vclight ,
light.5 = 3, -36.64, 0.00, 10.50, fx_navWhi ,
//light.6 = 3, 8.50, 0.00, 4.72, fx_navWhi ,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.0
master_ignition_switch = 1
engine.0 = 6.66, -9.86, -1.32,
engine.1 = 14.31, 0, 0,
engine.2 = 6.66, 9.60, -1.18,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt_jenny
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 3
electric_pump = 0
Center1 = -1, 0, 3.6, 31, 0
LeftMain = -1, -5.9, 3.6, 100, 0
RightMain = -1, 5.9, 3.6, 100, 0
[contact_points]
static_pitch = 11
static_cg_height = 8
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7
point.0 = 1, -29.9542, 0, -2.5168, 1200, 0, 0.74, 22, 0.24, 2.5, 0.695, 5, 5, 0, 0, 0
point.1 = 1, 2.0727, -9.6956, -9.1197, 1600, 1, 1.53, 0, 0.504, 2.5, 0.686, 5, 5, 2, 0, 0
point.2 = 1, 2.0223, 9.828, -9.1197, 1600, 2, 1.53, 0, 0.504, 2.5, 0.682, 5, 5, 3, 0, 0
point.3 = 2, -1.6, -40.7443, 4.2073, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.6, 40.4802, 3.9432, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -36.0, 0.0, 10.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.6 = 2, 14.7833, 0, -3.5992, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000
[airplane_geometry]
wing_area = 1033
wing_span = 84.56
wing_root_chord = 16.00
wing_dihedral = 3
wing_incidence = 2.0
wing_twist = 0.0
oswald_efficiency_factor = 0.9
wing_winglets_flag = 0
wing_sweep = 3
wing_pos_apex_lon = 4.26
wing_pos_apex_vert = 3.37
htail_area = 114.0
htail_span = 23.28
htail_pos_lon = -28.69
htail_pos_vert = 1.64
htail_incidence = 0.0
htail_sweep = 25
vtail_area = 61.0
vtail_span = 9.39
vtail_sweep = 44
vtail_pos_lon = -32.40
vtail_pos_vert = 6.09
elevator_area = 46.0
aileron_area = 25.6
rudder_area = 15.0
elevator_up_limit = 30.0
elevator_down_limit = 20.0
aileron_up_limit = 20.0
aileron_down_limit = 20.0
rudder_limit = 30.0
elevator_trim_limit = 19.5
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
[electrical]
max_battery_voltage = 12
generator_alternator_voltage = 13
max_generator_alternator_amps = 25
engine_generator_map = 0,1,0
electric_always_available = 0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
p_factor_on_yaw = 0.5
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=4.000000
system_type=0
flaps-position.0 = 0.0
flaps-position.1 = 10.0
flaps-position.2 = 25.0
flaps-position.3 = 40.0
damaging-speed = 500
blowout-speed = 500
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 3
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=202 //Cubic inches per cylinder
compression_ratio=6.5 //Compression ratio
number_of_cylinders=9 //Number of cylinders
max_rated_rpm=2200 //Max rated RPM
max_rated_hp=650 //Max rated HP
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3 //Starter torque factor
turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=0 //Max design manifold pressure, (inHg)
min_design_mp=0 //Min design manifold pressure, (inHg)
critical_altitude=0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=10.5 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=6.3 //Propeller moment of inertia
beta_max=0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400 //Miminum governed RPM
prop_tc=0.0 //Prop time-constant
gear_reduction_ratio=1.0 //Propeller gear reduction ratio
fixed_pitch_beta=25 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=0 //Minimum RPM for prop feathering
beta_feather=0 //Feathering pitch angle (degrees)
power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller by feathered prop
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees)
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.7 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint=6.46, 0.0, 3.26
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=0
Com.1=1, 0
Nav.1=0, 0, 0
Adf.1=0
Transponder.1=0
Marker.1=0
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=0,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
[Reference Speeds]
flaps_up_stall_speed=50.4 //Knots True (KTAS)
full_flaps_stall_speed=50.4 //Knots True (KTAS)
cruise_speed=140 //Knots True (KTAS)
max_indicated_speed = 190 //Red line (KIAS)
[autopilot]
autopilot_available=0
flight_director_available=0
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[stall_warning]
type=1
